GB1114414A - Improvements in space vehicles - Google Patents
Improvements in space vehiclesInfo
- Publication number
- GB1114414A GB1114414A GB23219/64A GB2321964A GB1114414A GB 1114414 A GB1114414 A GB 1114414A GB 23219/64 A GB23219/64 A GB 23219/64A GB 2321964 A GB2321964 A GB 2321964A GB 1114414 A GB1114414 A GB 1114414A
- Authority
- GB
- United Kingdom
- Prior art keywords
- module
- stage
- modules
- assembly
- fuel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 239000000446 fuel Substances 0.000 abstract 3
- 238000000926 separation method Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/14—Space shuttles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Transportation (AREA)
- Transmission Devices (AREA)
- Toys (AREA)
- Buildings Adapted To Withstand Abnormal External Influences (AREA)
Abstract
1,114,414. Space vehicles. BRITISH AIRCRAFT CORPORATION (OPERATING) Ltd. 16 June, 1965 [18 June, 1964], No. 23219/64. Heading B7W. A space vehicle which includes a final stage intended to travel beyond the earth's atmosphere, and a first stage intended to accompany the final stage during the first part of launching, and then become separated from it, comprises an assembly of components grouped together, including at least two modules which are shaped so that individually they are capable of flight in the atmosphere with substantial aerodynamic lift, each module of the first stage having a similar delta planform, with an elongated nose and a deep cross-section to accommodate large quantities of fuel, and having identical basic structure and each module of the first stage having a rear propulsion nozzle so placed in the assembly that it can operate prior to separation of the stages from one another. Each module comprises a lifting body of considerable depth to accommodate fuel, the under surface 32 being so shaped that three such modules may be connected together in an assembly (Figs. 2X, 2Y, not shown). A fixed fin 26 and outwardly-pivoting fins 28 and an adjustable rocket propulsion unit 36 are provided. Two modules comprise the first stage and the other the final stage, apparatus (Figs. 17A, 17B, not shown) being described for connecting the modules together and for transferring fuel from one module to another. Other shapes of module and arrangements of grouping to form first and subsequent stages are described.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB23219/64A GB1114414A (en) | 1964-06-18 | 1964-06-18 | Improvements in space vehicles |
| US464481A US3369771A (en) | 1964-06-18 | 1965-06-16 | Space vehicles |
| DE19651456202 DE1456202B2 (en) | 1964-06-18 | 1965-06-16 | MULTI-STAGE SPACE VEHICLE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB23219/64A GB1114414A (en) | 1964-06-18 | 1964-06-18 | Improvements in space vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1114414A true GB1114414A (en) | 1968-05-22 |
Family
ID=10192091
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB23219/64A Expired GB1114414A (en) | 1964-06-18 | 1964-06-18 | Improvements in space vehicles |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US3369771A (en) |
| DE (1) | DE1456202B2 (en) |
| GB (1) | GB1114414A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2161108C1 (en) * | 2000-02-07 | 2000-12-27 | Государственный космический научно-производственный центр им. М.В. Хруничева | Method for orbit injection of payload by multifunctional launch vehicle of combination arrangement with cruise liquid- propellant rocket engine installations (lrei), multifunctional launch vehicle with cruise lpei and method for its development |
| RU2232700C2 (en) * | 2001-09-05 | 2004-07-20 | Гашимов Мирсултан Исмаил-оглы | Method of injection of objects into near-earth orbit and recoverable aero-space rocket aircraft-carrier for realization of this method (aero-space system nur-said system) |
| RU2291817C2 (en) * | 2002-06-14 | 2007-01-20 | Михаил Владимирович Михальчук | Module-type launch vehicle (versions) |
| RU2321526C1 (en) * | 2006-08-04 | 2008-04-10 | Открытое акционерное общество "Научно-производственное объединение "МОЛНИЯ" | Launch vehicle recoverable booster |
| RU2337040C2 (en) * | 2006-08-28 | 2008-10-27 | Мирсултан Исмаил оглы Гашимов | Lunar complex with reusable elements, earth-moon-earth transportation system and method to this effect |
| RU2438940C2 (en) * | 2009-07-31 | 2012-01-10 | Мицубиси Хэви Индастриз, Лтд. | Launching system and installation |
| DE102012000243A1 (en) * | 2012-01-09 | 2013-07-11 | Jerg Jaisle | Gliding flight device for transporting loads, has fuselage element for receiving loads, delta wing for generating lifting force and control element for influencing aircraft movement of gliding flight device in flight |
Families Citing this family (49)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3534924A (en) * | 1967-09-07 | 1970-10-20 | Nasa | Variable geometry manned orbital vehicle |
| US3700193A (en) * | 1971-01-14 | 1972-10-24 | Nasa | A method of delivering a vehicle to earth orbit and returning the reusable portion thereof to earth |
| US3929306A (en) * | 1974-03-05 | 1975-12-30 | Nasa | Space vehicle system |
| US4265416A (en) * | 1978-05-30 | 1981-05-05 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Orbiter/launch system |
| US4354646A (en) * | 1978-09-20 | 1982-10-19 | Rockwell International Corporation | Variable dihedral angle tail unit for supersonic aircraft |
| US4451017A (en) * | 1982-09-30 | 1984-05-29 | The United States Of America As Represented By The Administrator, National Aeronautics And Space Administration | Three stage rocket vehicle with parallel staging |
| US4834324A (en) * | 1983-11-07 | 1989-05-30 | Criswell David R | Multiconfiguration reusable space transportation system |
| US5217187A (en) * | 1983-11-07 | 1993-06-08 | Criswell David R | Multi-use launch system |
| US4609169A (en) * | 1984-08-14 | 1986-09-02 | The United States Of America As Represented By The Secretary Of The Air Force | Propellant tank resupply system |
| US4802639A (en) * | 1984-09-28 | 1989-02-07 | The Boeing Company | Horizontal-takeoff transatmospheric launch system |
| US4699339A (en) * | 1985-03-01 | 1987-10-13 | Hughes Aircraft Company | Apparatus and method for transporting a spacecraft and a fluid propellant from the earth to a substantially low gravity environment above the earth |
| US4817895A (en) * | 1985-06-18 | 1989-04-04 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Aerobraking orbital transfer vehicle |
| US4741502A (en) * | 1985-10-01 | 1988-05-03 | Hughes Aircraft Company | Method and apparatus for launching a spacecraft by use of a recoverable upper rocket stage |
| US4796839A (en) * | 1987-01-08 | 1989-01-10 | Davis Hubert P | Space launch vehicle |
| US5141181A (en) * | 1989-10-05 | 1992-08-25 | Leonard Byron P | Launch vehicle with interstage propellant manifolding |
| US5129602A (en) * | 1989-10-05 | 1992-07-14 | Leonard Byron P | Multistage launch vehicle employing interstage propellant transfer and redundant staging |
| US5143328A (en) * | 1989-10-05 | 1992-09-01 | Leonard Byron P | Launch vehicle with reconfigurable interstage propellant manifolding and solid rocket boosters |
| US5203844A (en) * | 1989-10-05 | 1993-04-20 | Leonard Byron P | Multiple payload/failure mode launch vehicles |
| US5143327A (en) * | 1990-08-31 | 1992-09-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Integrated launch and emergency vehicle system |
| US5217188A (en) * | 1991-04-08 | 1993-06-08 | Trw Inc. | Modular solid-propellant launch vehicle and related launch facility |
| US5295642A (en) * | 1991-11-08 | 1994-03-22 | Spread Spectrum, Inc. | High altitude launch platform payload launching apparatus and method |
| RU2116941C1 (en) * | 1997-01-10 | 1998-08-10 | Белянин Эдуард Валентинович | Multistage launch vehicle |
| US6360994B2 (en) | 1997-12-19 | 2002-03-26 | Don A. Hart & Associates, Inc. | Configurable space launch system |
| US6612522B1 (en) * | 1998-03-17 | 2003-09-02 | Starcraft Boosters, Inc. | Flyback booster with removable rocket propulsion module |
| US6446905B1 (en) * | 2000-08-30 | 2002-09-10 | The Aerospace Corporation | Janus reusable spacecraft system |
| US6685141B2 (en) * | 2001-03-28 | 2004-02-03 | The Aerospace Corporation | X33 aeroshell and bell nozzle rocket engine launch vehicle |
| GB2377683A (en) * | 2001-07-20 | 2003-01-22 | Bae Systems Plc | Composite of unmanned aerial vehicles |
| US20030052232A1 (en) * | 2001-09-17 | 2003-03-20 | Hall Allison Earl | Space transportation system |
| US6932302B2 (en) * | 2002-12-19 | 2005-08-23 | The Boeing Company | Reusable launch system |
| US20060226295A1 (en) * | 2005-03-25 | 2006-10-12 | Gulick Douglas S | Lifting body tuned for passive re-entry |
| FR2902762B1 (en) * | 2006-06-27 | 2009-07-10 | Eads Astrium Sas Soc Par Actio | METHOD FOR OPERATING ORBIT OF AN ARTIFICIAL SATELLITE AND ASSOCIATED PROPULSION DEVICE |
| US20080105783A1 (en) * | 2006-11-03 | 2008-05-08 | Cessna Aircraft Company | Fuselage design for sonic boom suppression of supersonic aircraft |
| RU2331550C1 (en) * | 2007-01-09 | 2008-08-20 | Федеральное государственное унитарное предприятие Государственный научно-производственный ракетно-космический центр "ЦСКБ-ПРОГРЕСС" (ФГУП ГНПРКЦ "ЦСКБ-ПРОГРЕСС") | Carrier rocket |
| RU2385275C1 (en) * | 2009-02-20 | 2010-03-27 | Александр Олегович Майборода | Method for transfer of working fluid for engines of spacecrafts and system of its implementation |
| ES2378202B1 (en) * | 2009-03-17 | 2013-02-28 | Fº JAVIER PORRAS VILA | LAUNCHER OF PROPELLERS WITH MULTIPLIER GEAR. |
| US8528853B2 (en) * | 2010-07-29 | 2013-09-10 | David I. Luther | In-line staged horizontal takeoff and landing space plane |
| US9073647B2 (en) | 2013-04-25 | 2015-07-07 | Biosphere Aerospace Llc | Space shuttle orbiter and return system |
| US9758247B2 (en) * | 2014-06-10 | 2017-09-12 | Sikorsky Aircraft Corporation | Combined launch and mission vehicles |
| USD856897S1 (en) * | 2017-12-15 | 2019-08-20 | Katholieke Universiteit Leuven, K.U.Leuven R&D | Vertical takeoff and landing unmanned aerial vehicle |
| US10807013B2 (en) | 2017-12-20 | 2020-10-20 | Francis A. Alonso | Modified delta wing kite with inflatable fuselage |
| USD866394S1 (en) * | 2018-01-30 | 2019-11-12 | GEOSAT Aerospace & Technology | Unmanned aerial vehicle |
| US20190351994A1 (en) * | 2018-05-16 | 2019-11-21 | Richard Michael Truhill | Retractable aircraft control surface |
| USD874577S1 (en) * | 2018-08-23 | 2020-02-04 | Francis A. Alonso | Swept wing kite |
| USD875183S1 (en) * | 2018-08-23 | 2020-02-11 | Francis A. Alonso | Zig-zagged swept wing kite |
| USD874578S1 (en) * | 2018-08-23 | 2020-02-04 | Francis A. Alonso | Swept wing kite |
| USD873350S1 (en) * | 2018-08-23 | 2020-01-21 | Francis A. Alonso | Zig-zagged swept wing kite |
| RU2730300C9 (en) * | 2018-11-02 | 2021-06-22 | Владимир Федорович Петрищев | Device for mass delivery of tourists to stratosphere and subsequent return to ground |
| RU2717406C1 (en) * | 2019-04-12 | 2020-03-23 | Виктор Георгиевич Карелин | Reusable space system and method for control thereof |
| RU2742908C2 (en) * | 2019-04-26 | 2021-02-11 | Акционерное общество "Государственный ракетный центр имени академика В.П. Макеева" | Space rocket |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB696751A (en) * | 1949-01-25 | 1953-09-09 | Fairey Aviat Co Ltd | Improvements in or relating to flying bodies |
| US2792784A (en) * | 1950-10-27 | 1957-05-21 | Bristol Aeroplane Co Ltd | Prime movers |
| US3104079A (en) * | 1960-10-07 | 1963-09-17 | William H Phillips | Variable-geometry winged reentry vehicle |
| US3132825A (en) * | 1961-09-25 | 1964-05-12 | Bell Aerospace Corp | Space-atmosphere vehicle |
| US3202381A (en) * | 1961-11-08 | 1965-08-24 | Hans F Wuenscher | Recoverable rocket vehicle |
| US3276722A (en) * | 1964-02-04 | 1966-10-04 | Jr Alfred J Eggers | Flight craft |
-
1964
- 1964-06-18 GB GB23219/64A patent/GB1114414A/en not_active Expired
-
1965
- 1965-06-16 US US464481A patent/US3369771A/en not_active Expired - Lifetime
- 1965-06-16 DE DE19651456202 patent/DE1456202B2/en active Pending
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1837277A2 (en) | 2000-02-07 | 2007-09-26 | FGUP "Gosudarstvenny Kosmichesky Nauchno-Proizvodstvenny Tsentr imeni M.V. Khrunicheva" | Multifunctional launch vehicle of combined scheme with cruise liquid rocket engine systems (LRESs) |
| WO2001056880A1 (en) | 2000-02-07 | 2001-08-09 | Gosudarstvenny Kosmichesky Nauchno-Proizvodstvennytsentr Im. M.V.Khrunicheva | Method for placing a payload into orbit by means of a hybrid multifunction booster rocket equipped with a liquid-fuel rocket propulsion system (lrps), hybrid multifunction booster rocket with cruising lrps and development test therefor |
| US6581881B2 (en) | 2000-02-07 | 2003-06-24 | Gosudarstvenny Kosmichesky Nauchno-Proizvodstvenny Tsentr Im. M. V. | Method for placing payload in orbit by multifunctional launch vehicle of combined scheme with cruise liquid rocket engine system (lres), multifunctional launch vehicle of combined scheme with cruise lres and method for refining it |
| US6712319B2 (en) | 2000-02-07 | 2004-03-30 | Gosudarstvenny Kosmichesky Nauchno-Proizvodstvenny Tsentr Tm. M.V. Khrunicheva | Method for placing payload in orbit by multifunctional launch vehicle of combined scheme with cruise liquid rocket engine system (lres), multifunctional launch vehicle of combined scheme with cruise lres and method of refining it |
| US6769651B2 (en) | 2000-02-07 | 2004-08-03 | Federalnoe Gosudarstvennoe Unitarnoe Predpriyatie Gosudarstvenny Kosmichesky Nauchno-Proizvodstvenny Tsentr Im.M.V. Krunicheva | Method for placing payload in orbit by multifunctional launch vehicle of combined scheme with cruise liquid rocket engine system (lres), multifunctional launch vehicle of combined scheme with cruise lres and method for refining it |
| RU2161108C1 (en) * | 2000-02-07 | 2000-12-27 | Государственный космический научно-производственный центр им. М.В. Хруничева | Method for orbit injection of payload by multifunctional launch vehicle of combination arrangement with cruise liquid- propellant rocket engine installations (lrei), multifunctional launch vehicle with cruise lpei and method for its development |
| RU2232700C2 (en) * | 2001-09-05 | 2004-07-20 | Гашимов Мирсултан Исмаил-оглы | Method of injection of objects into near-earth orbit and recoverable aero-space rocket aircraft-carrier for realization of this method (aero-space system nur-said system) |
| RU2291817C2 (en) * | 2002-06-14 | 2007-01-20 | Михаил Владимирович Михальчук | Module-type launch vehicle (versions) |
| RU2321526C1 (en) * | 2006-08-04 | 2008-04-10 | Открытое акционерное общество "Научно-производственное объединение "МОЛНИЯ" | Launch vehicle recoverable booster |
| RU2337040C2 (en) * | 2006-08-28 | 2008-10-27 | Мирсултан Исмаил оглы Гашимов | Lunar complex with reusable elements, earth-moon-earth transportation system and method to this effect |
| RU2438940C2 (en) * | 2009-07-31 | 2012-01-10 | Мицубиси Хэви Индастриз, Лтд. | Launching system and installation |
| US8262015B2 (en) | 2009-07-31 | 2012-09-11 | Mitsubishi Heavy Industries, Ltd. | Launching system and launching apparatus |
| DE102012000243A1 (en) * | 2012-01-09 | 2013-07-11 | Jerg Jaisle | Gliding flight device for transporting loads, has fuselage element for receiving loads, delta wing for generating lifting force and control element for influencing aircraft movement of gliding flight device in flight |
| DE102012000243B4 (en) | 2012-01-09 | 2019-10-10 | Jerg Jaisle | Glider for transporting loads and method for operating the glider |
Also Published As
| Publication number | Publication date |
|---|---|
| DE1456202B2 (en) | 1971-11-18 |
| DE1456202A1 (en) | 1969-02-06 |
| US3369771A (en) | 1968-02-20 |
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